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Nonlinear rotordynamics analysisThe special nonlinearities of the Jeffcott equations in rotordynamics are examined. The immediate application of this analysis is directed toward understanding the excessive vibrations recorded in the LOX pump of the SSME during hot firing ground testing. Deadband, side force and rubbing are three possible sources of inducing nonlinearity in the Jeffcott equations. The present analysis initially reduces these problems to the same mathematical description. A special frequency, named the nonlinear natural frequency is defined and used to develop the solutions of the nonlinear Jeffcott equations as asympotic expansions. This nonlinear natural frequency which is the ratio of the cross-stiffness and the damping, plays a major role in determining response frequencies. Numerical solutions are included for comparison with the analysis. Also, nonlinear frequency-response tables are made for a typical range of values.
Document ID
19850014053
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Day, W. B.
(Auburn Univ. AL, United States)
Date Acquired
September 5, 2013
Publication Date
March 15, 1985
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-171425
NAS 1.26:171425
Report Number: NASA-CR-171425
Report Number: NAS 1.26:171425
Accession Number
85N22364
Funding Number(s)
CONTRACT_GRANT: NAS8-35992
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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